Harman Patil (Editor)

Piper J 4

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Top speed
  
161 km/h

Length
  
6.7 m

Engine type
  
Number of seats
  
2

Wingspan
  
11 m

Introduced
  
1938

Manufacturer
  
Piper J-4 Piper J4 Cub Coupe airplane pictures J4A J4B J4E J4F L4E

The Piper J-4 Cub Coupe is a two place side-by-side version of the Piper J-3 that was built between 1938 and 1942 by Piper Aircraft. It was Piper's first model with side-by-side seating; combined with docile low-speed handling, this made it a good trainer.

Contents

Piper J-4 J4 Cub CoupePIPER J4 L1P L

J-4 development

Piper J-4 Piper J4 Cub Coupe Untitled Aviation Photo 2471419 Airlinersnet

The fuselage of the J-4 was wider than the J-3 and the aircraft had a fully enclosed rear decking to the fuselage top. The first J-4s had a Continental 50 hp A50 engine, with up exhaust, an open cowl, oil and spring landing gear, a modified tail wheel system and many other changes. The early J-4 had a comfortable cockpit but was slower than most side by side aircraft of the day.

Piper J-4 J4 Cub Coupe Pilot Report

The 1940 J-4A gained a fully enclosed cowling, a Continental 65 hp A65 engine, and aft auxiliary fuel. The J-4B was fitted with a 60 hp Franklin 4AC-171 engine. The final version was the 1941 J-4E which sported a 75 hp Continental engine and redesigned interior. The main fuel tank was moved to the wing along with a header tank. Performance was now on par with similar contemporary types, but the attack on Pearl Harbor sealed its fate as all civilian aircraft manufacture came to a stop with the entry of the United States into World War II.

Piper J-4 Piper J4 Cub Coupe airplane pictures J4A J4B J4E J4F L4E

Some J-4s had another unique feature in the tail construction: the stabilizer was made of stainless steel tubing, riveted together with gussets.

Variants

Piper J-4 wwwaviastarorgpicturesusapiperj4jpg
J-4
powered by a 50-hp (37-kW) Continental A50-1 piston engine.
J-4A
powered by a 65-hp (48-kW) Continental A65-1 or -8 piston engine.
J-4B
powered by a 60-hp (45-kW) Franklin 4AC-171 or 65-hp (48-kW) 4AC-176-B2 piston engine.
J-4E
powered by a 75-hp (56-kW) Continental A75-9 piston engine.
J-4F
powered by a 55-hp (41-kW) Avco Lycoming 0-145-A1, -A2 or 65-hp (48-kW) 0-145-B1 piston engine.

Specification (J-4A)

Data from Simpson, 2001, p. 430.

General characteristics

Piper J-4 Piper J4

  • Length: 22 ft 6 in (6.86 m)
  • Wingspan: 36 ft 2 in (11.02 m)
  • Height: 6 ft 10 in (2.08 m)
  • Gross weight: 1300 lb (589.67 kg)
  • Powerplant: 1 × Continental A65-1 piston engine, 65 hp ( kW) each
  • Performance

  • Maximum speed: 100 mph (160.93 km/h)
  • Cruise speed: 92 mph (148.06 km/h)
  • Range: 360 miles (579.36 km)
  • Service ceiling: 15,000 ft (4572 m)
  • Rate of climb: 600 ft/min (3.04 m/s)
  • References

    Piper J-4 Wikipedia


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